TY - JOUR
T1 - Planar Smooth Path Guidance Law for a Small Unmanned Aerial Vehicle with Parameter Tuned by Fuzzy Logic
AU - Chen, Yang
AU - Liang, Jianhong
AU - Wang, Chaolei
AU - Zhang, Yicheng
AU - Wang, Tianmiao
AU - Xue, Chenghao
N1 - Publisher Copyright:
© 2017 Yang Chen et al.
PY - 2017
Y1 - 2017
N2 - A guidance law has been designed to guide the small unmanned aerial vehicle towards the predefined horizontal smooth path. The guidance law only needs the mathematical expression for the predefined path, the positions, and the velocities of the vehicle in the horizontal inertial frame. The stability of the guidance law has been demonstrated by the Lyapunov stability arguments. In order to improve the path following performance, one of the parameters of the guidance law is tuned by using the fuzzy logic which will still keep its stability. The simulation experiments in the Matlab/Simulink environment to realize the square-, circular-, and the athletics track-style paths following are given to verify the effectiveness of the proposed method. The simulation results show that the path following performance will be improved with smaller overshoot and oscillation amplitude and shorter arrival time with the parameter tuned.
AB - A guidance law has been designed to guide the small unmanned aerial vehicle towards the predefined horizontal smooth path. The guidance law only needs the mathematical expression for the predefined path, the positions, and the velocities of the vehicle in the horizontal inertial frame. The stability of the guidance law has been demonstrated by the Lyapunov stability arguments. In order to improve the path following performance, one of the parameters of the guidance law is tuned by using the fuzzy logic which will still keep its stability. The simulation experiments in the Matlab/Simulink environment to realize the square-, circular-, and the athletics track-style paths following are given to verify the effectiveness of the proposed method. The simulation results show that the path following performance will be improved with smaller overshoot and oscillation amplitude and shorter arrival time with the parameter tuned.
UR - https://www.scopus.com/pages/publications/85018654434
U2 - 10.1155/2017/6712602
DO - 10.1155/2017/6712602
M3 - 文章
AN - SCOPUS:85018654434
SN - 1687-5249
VL - 2017
JO - Journal of Control Science and Engineering
JF - Journal of Control Science and Engineering
M1 - 6712602
ER -